The Two-Dimensional Supersonic Flow and Mixing with a Perpendicular Injection in a Scramjet Combustor
Mohammad Ali ; S. Ahmed ; A.K.M. Sadrul Islam
刊名JOURNAL OF THERMAL SCIENCE
2003
卷号12期号:4页码:371,380
关键词scramjet engine TVD scheme finite width of inlet supersonic mixing parallel air stream flame holding.
公开日期2013-03-12
内容类型期刊论文
源URL[http://ir.etp.ac.cn/handle/311046/53520]  
专题工程热物理研究所_Journal of Thermal Science_期刊论文
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GB/T 7714
Mohammad Ali,S. Ahmed,A.K.M. Sadrul Islam. The Two-Dimensional Supersonic Flow and Mixing with a Perpendicular Injection in a Scramjet Combustor[J]. JOURNAL OF THERMAL SCIENCE,2003,12(4):371,380.
APA Mohammad Ali,S. Ahmed,&A.K.M. Sadrul Islam.(2003).The Two-Dimensional Supersonic Flow and Mixing with a Perpendicular Injection in a Scramjet Combustor.JOURNAL OF THERMAL SCIENCE,12(4),371,380.
MLA Mohammad Ali,et al."The Two-Dimensional Supersonic Flow and Mixing with a Perpendicular Injection in a Scramjet Combustor".JOURNAL OF THERMAL SCIENCE 12.4(2003):371,380.
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